A high-efficiency aerothermoelastic analysis method
In this paper, a high-efficiency aerothermoelastic analysis method based on unified hypersonic lifting surface theory is estab- lished. The method adopts a two-way coupling form that couples the structure, aerodynamic force, and aerodynamic thermo and heat conduction. The aerodynamic force is first...
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Published in | Science China. Physics, mechanics & astronomy Vol. 57; no. 6; pp. 1111 - 1118 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Heidelberg
Science China Press
01.06.2014
Springer Nature B.V |
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Abstract | In this paper, a high-efficiency aerothermoelastic analysis method based on unified hypersonic lifting surface theory is estab- lished. The method adopts a two-way coupling form that couples the structure, aerodynamic force, and aerodynamic thermo and heat conduction. The aerodynamic force is first calculated based on unified hypersonic lifting surface theory, and then the Eckert reference temperature method is used to solve the temperature field, where the transient heat conduction is solved using Fourier's law, and the modal method is used for the aeroelastic correction. Finally, flutter is analyzed based on the p-k method. The aerothermoelastic behavior of a typical hypersonic low-aspect ratio wing is then analyzed, and the results indicate the fol- lowing: (1) the combined effects of the aerodynamic load and thermal load both deform the wing, which would increase if the flexibility, size, and flight time of the hypersonic aircraft increase; (2) the effect of heat accumulation should be noted, and therefore, the trajectory parameters should be considered in the design of hypersonic flight vehicles to avoid hazardous condi- tions, such as flutter. |
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AbstractList | In this paper, a high-efficiency aerothermoelastic analysis method based on unified hypersonic lifting surface theory is estab- lished. The method adopts a two-way coupling form that couples the structure, aerodynamic force, and aerodynamic thermo and heat conduction. The aerodynamic force is first calculated based on unified hypersonic lifting surface theory, and then the Eckert reference temperature method is used to solve the temperature field, where the transient heat conduction is solved using Fourier's law, and the modal method is used for the aeroelastic correction. Finally, flutter is analyzed based on the p-k method. The aerothermoelastic behavior of a typical hypersonic low-aspect ratio wing is then analyzed, and the results indicate the fol- lowing: (1) the combined effects of the aerodynamic load and thermal load both deform the wing, which would increase if the flexibility, size, and flight time of the hypersonic aircraft increase; (2) the effect of heat accumulation should be noted, and therefore, the trajectory parameters should be considered in the design of hypersonic flight vehicles to avoid hazardous condi- tions, such as flutter. In this paper, a high-efficiency aerothermoelastic analysis method based on unified hypersonic lifting surface theory is established. The method adopts a two-way coupling form that couples the structure, aerodynamic force, and aerodynamic thermo and heat conduction. The aerodynamic force is first calculated based on unified hypersonic lifting surface theory, and then the Eckert reference temperature method is used to solve the temperature field, where the transient heat conduction is solved using Fourier’s law, and the modal method is used for the aeroelastic correction. Finally, flutter is analyzed based on the p-k method. The aerothermoelastic behavior of a typical hypersonic low-aspect ratio wing is then analyzed, and the results indicate the following: (1) the combined effects of the aerodynamic load and thermal load both deform the wing, which would increase if the flexibility, size, and flight time of the hypersonic aircraft increase; (2) the effect of heat accumulation should be noted, and therefore, the trajectory parameters should be considered in the design of hypersonic flight vehicles to avoid hazardous conditions, such as flutter. |
Author | WAN ZhiQiang WANG YaoKun LIU YunZhen YANG Chao |
AuthorAffiliation | School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China |
Author_xml | – sequence: 1 givenname: ZhiQiang surname: Wan fullname: Wan, ZhiQiang organization: School of Aeronautic Science and Engineering, Beihang University – sequence: 2 givenname: YaoKun surname: Wang fullname: Wang, YaoKun organization: School of Aeronautic Science and Engineering, Beihang University – sequence: 3 givenname: YunZhen surname: Liu fullname: Liu, YunZhen organization: School of Aeronautic Science and Engineering, Beihang University – sequence: 4 givenname: Chao surname: Yang fullname: Yang, Chao email: yangchao@buaa.edu.cn organization: School of Aeronautic Science and Engineering, Beihang University |
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Cites_doi | 10.2514/1.J050193 10.2514/2.2316 10.2514/3.46801 10.2514/8.2657 10.1007/s11431-011-4722-4 10.2514/2.2199 10.2514/1.J050882 10.1016/S0376-0421(03)00079-4 |
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Keywords | flutter two-way coupling aerothermoelastic unified hypersonic lifting surface theory piston theory |
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Notes | 11-5000/N In this paper, a high-efficiency aerothermoelastic analysis method based on unified hypersonic lifting surface theory is estab- lished. The method adopts a two-way coupling form that couples the structure, aerodynamic force, and aerodynamic thermo and heat conduction. The aerodynamic force is first calculated based on unified hypersonic lifting surface theory, and then the Eckert reference temperature method is used to solve the temperature field, where the transient heat conduction is solved using Fourier's law, and the modal method is used for the aeroelastic correction. Finally, flutter is analyzed based on the p-k method. The aerothermoelastic behavior of a typical hypersonic low-aspect ratio wing is then analyzed, and the results indicate the fol- lowing: (1) the combined effects of the aerodynamic load and thermal load both deform the wing, which would increase if the flexibility, size, and flight time of the hypersonic aircraft increase; (2) the effect of heat accumulation should be noted, and therefore, the trajectory parameters should be considered in the design of hypersonic flight vehicles to avoid hazardous condi- tions, such as flutter. aerothermoelastic, two-way coupling, unified hypersonic lifting surface theory, piston theory, flutter ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
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PublicationDate | 2014-06-01 |
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PublicationTitle | Science China. Physics, mechanics & astronomy |
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PublicationYear | 2014 |
Publisher | Science China Press Springer Nature B.V |
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References | Bertin, Cummings (CR21) 2003; 39 Karpel, Presente (CR20) 1995; 32 Yang, Xu, Xie (CR1) 2010; 31 Huang, Wang (CR2) 2009; 5 Karpel (CR22) 1998; 35 Biedron, Rumsey (CR24) 1998 McNamara, Friedmann (CR9) 2011; 49 Qian (CR23) 2004 Watkins, Berman (CR18) 1955 Liu, Yao, Sarhaddi (CR16) 1997; 34 McNamara (CR5) 2005 Wu, Hui, Yang (CR6) 2005; 31 Chen, Xu, Cai (CR7) 2012; 30 Lighthill (CR15) 2012; 20 Yang, Tao (CR14) 2007 Culler, McNamara (CR11) 2010 Eckert (CR13) 1956; 78 Liu, Chen, Tang (CR17) 2002 Garrick (CR4) 1963; 22 McNamara, Culler, Crowell (CR8) 2009 Yang, Li, Wan (CR12) 2012; 55 Culler, McNamara (CR10) 2010; 48 Yang, Wu, Wan (CR3) 2011 Qu, Liu, Zeng (CR19) 2000 M Karpel (5410_CR20) 1995; 32 C E Watkins (5410_CR18) 1955 Z G Wu (5410_CR6) 2005; 31 C Yang (5410_CR1) 2010; 31 I E Garrick (5410_CR4) 1963; 22 D D Liu (5410_CR17) 2002 S Y Huang (5410_CR2) 2009; 5 A J Culler (5410_CR11) 2010 H Chen (5410_CR7) 2012; 30 E R G Eckert (5410_CR13) 1956; 78 M J Lighthill (5410_CR15) 2012; 20 J J McNamara (5410_CR8) 2009 R T Biedron (5410_CR24) 1998 Z H Qu (5410_CR19) 2000 M Karpel (5410_CR22) 1998; 35 J J Bertin (5410_CR21) 2003; 39 D D Liu (5410_CR16) 1997; 34 J J McNamara (5410_CR9) 2011; 49 J J McNamara (5410_CR5) 2005 C Yang (5410_CR12) 2012; 55 C Yang (5410_CR3) 2011 A J Culler (5410_CR10) 2010; 48 Y J Qian (5410_CR23) 2004 S M Yang (5410_CR14) 2007 |
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SubjectTerms | Aerodynamic forces Aerodynamic loads Aspect ratio Astronomy Classical and Continuum Physics Conduction heating Conductive heat transfer Deformation effects Flight time Flight vehicles Flutter Flutter analysis Heat Hypersonic aircraft Hypersonic flight Hypersonic flow Lift devices Lifting surfaces Observations and Techniques Physics Physics and Astronomy Temperature distribution Thermal analysis Transient heat conduction Vibration Wings (aircraft) 傅立叶定律 升力面理论 双向耦合 模态方法 气动弹性 瞬态热传导 高超声速飞行器 高超音速飞行器 |
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Title | A high-efficiency aerothermoelastic analysis method |
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